GE CF6-80C2A5

Service difficulty reports · 164

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'CF680C2A5'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AALA20050486Duct · leakingMIA - INFLIGHT ON MAX POWER TAKEOFF ENGINE EXHAUST TEMPERATURE REACHED 1000. AFTER LIFT OFF ATTEMPTED TO RETARD NUMBER 2 THROTTLE BUT IT WAS STUCK FORWARD. RECEIVED INTERMITTENT OVERTEMP AND FIRE INDICATION. RAN FIRE PROCEDURE AND SHOT BOTH FIRE BOTTLES IN Jul 30, 2005 · N7083A · Airbus A300B4605R · Engine Bleed Air SystemSDR AALA20050463Engine · stalledON TAKEOFF NUMBER ONE ENGINE COMPRESSOR STALLED. RETUNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 22, 2005 · N7082A · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR AALA20050423Line · leakingYELLOW SYSTEM HYDRAULIC QUANTITY LOST ON CLIMB-OUT. FOUND HYDRAULIC LINE IN LT WHEEL WELL LEAKING. REPLACED HYDRAULIC LINE IN LT WHEEL WELL. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 3, 2005 · N11060 · Airbus A300B4605R · Hydraulic System, MainSDR AALA20050401Fuel Filter · contaminatedNR 1 ENGINE FUEL CLOG LIGHT CAME ON MOMENTARILY WITH CLIMB-OUT. INSPECTED ENGINE. REPLACED MAIN ENGINE FUEL FILTER ASSEMBLY AND DIFFERENTIAL PRESSURE SWITCH. OPERATIONAL CHECK NORMAL AND NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.Jun 22, 2005 · N70072 · Airbus A300B4605R · Engine Fuel DistributionSDR CA050610001Oven · sparks(CAN) CABIN CREW NOTICED SPARKS COMING FROM RT OVEN. OVEN WAS DEACTIVATED AND REPLACED AT THE NEXT MAINTENANCE STATION. OVEN ROUTED TO REPAIR SHOP FOR INVESTIGATION.Jun 2, 2005 · Airbus A310300 · Buffet/GalleysSDR CA050516008Inverter · failed(CAN) DURING FLIGHT DECK PREPARATION WITH EXTERNAL POWER OFF AND BATTERIES POWER ON, SMOKE ODOR WAS NOTICED IN FLIGHT DECK. DURING INVESTIGATION FOUND STATIC INVERTER AT FAULT WITH THE SUPPLIED FUSE BLOWN. BOTH UNITS WERE REPLACED. ALSO THIS POWER PROBLEM DISApr 26, 2005 · Airbus A310304 · AC InverterSDR CA050425009Push-Pull Cable · contaminated(CAN) WHILE IN CRUISE AT 340, AFTER 2.5 HRS IN FLIGHT, NR 2 ENGINE THROTTLE JAMMED. QRH APPLIED WING ANTI-ICE SELECTED. AFTER CRUISING AT 260, THROTTLE CONTROL RECOVERED AND NORMAL OPERATION UP TO FL 360 AND THE REMAINING OF THE FLIGHT. THROTTLE CONTROL VEApr 24, 2005 · Airbus A310300 · Power LeverSDR AALA20050241Fuel Control · inoperativeMCO - INABILITY TO FEED FORWARD TO ENGINES FROM INNER FUEL TANKS. ALL PUMPS OPERATE OK. REPLACED FUEL QUANTITY CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.Apr 3, 2005 · N40064 · Airbus A300B4605R · Fuel Control/Turbine EnginesSDR CA050301001Tube · odor(CAN) DURING PRE-DEPARTURE CHECK, ON THE GROUND, BURN SMELL WAS NOTICED FROM RT ECAM SYSTEM. DISPLAY UNIT WAS REMOVED AND INSPECTED. NO FAULT WAS FOUND AND SYSTEM WAS DEACTIVATED UNDER MEL. UNIT WAS REPLACED AT THE NEXT STATION. UNIT WAS SENT TO THE OEM FOR Feb 25, 2005 · Airbus A310304 · Central WarningSDR 05FDEA00062Bleed Valve · malfunctionedON CLIMBOUT NR 2 HP BLEED VALVE FAULTED, APP FL 280 LOSS BOTH PACKS. RESET OF PACKS AT 10,000 RESULTED IN NORMAL OPS. DID BITE CHECK OF PNEUMATIC CONTROLLERS, PER TSM 26-00-00, FAULTED NR 2 HP VALVE, DID BITE CHECK OF PACK CONTROLLER PER 21-60-00, NO FAULTSJan 10, 2005 · N654FE · Airbus A300F4605R · Compressor Bleed ValveSDR 04FDEA03006Seat Track · corrodedRT FR 40 TO 54, SEAT TRACK NR 3R HAS 8 AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK RAIL AT MDC RT FR 40 TO 44.5 NR 3 R IAW SRM 51-72-10.Nov 1, 2004 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03007Seat Track · corrodedFROM NR N00373 MCD FR 18, NR 3 RT SEAT TRACK HAS 1 AREA OF CORROSION ON SCALLOP HOLES AS MARKED. REPAIRED SEAT TRACK AT FR 18, NR 3, RT SIDE IAW SRM 53-12-16 BY CUTTING OUT OLD SECTION AND SPLICING NEW SECTION.Nov 1, 2004 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02984Warning Light · illuminatedPDIS 669 78-30 0007382 23OCT04 MEM CLOSE U LOGPAGES: 00926331 CLEARED FOR TAKE-OFF , STABILIZED ENGINES AT 40 PERE NT N1, THEN APPLIED TAKEOFF POWER. ALMOST IMMDEIATLY RECIEVED AMBER ECAM NR1 ENG REV PRESSURIZED REJECTED TAKEOFF AND RETURNED TO GATE. Oct 23, 2004 · N669FE · Airbus A300* · Engine Thrust ReverserSDR 04FDEA02985Adapter · corrodedRT FR.41-42, BETWEEN SEAT TRACKS NR 2 AND 3, CLS ADAPTER TRACK HAS CORROSION AT BOTH ENDS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED CLS ADAPTER IAW SRM 51-72-10.Oct 23, 2004 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 04FDEA02958Windshield · failed56-10 0007810 20OCT04 MEM CLOSE L/P: 00949119 CAPT FWD WINDSHIELD OUTER PANEL SHATTERED AT FL 310 REMOVED CAPTAINS WINDSHIELD REF A 300-600 MM 56-11-1 1-4. R/I IAW MM 56-11-11-4 MFG NP175201-1 SRL 96113H6246 ON MFG NP175201-5 SRL 04278H7866 AIRBUSOct 20, 2004 · N659FE · Airbus A300* · Flight Compartment WindowsSDR CA041020003Strut · lack of lube(CAN) ON APPROACH TO AIRPORT, FLIGHT CREW WAS UNABLE TO OBTAIN POSITIVE NOSE LANDING GEAR DOWN LOCK INDICATION EVEN AFTER SEVERAL CYCLES. A LANDING GEAR GRAVITY EXTENSION WAS CARRIED OUT SUCCESSFULLY.TROUBLE SHOOTING OF THE ELECTRICAL INDICATION SYSTEM DID NOTOct 16, 2004 · Airbus A310304 · Main Landing Gear Strut/Axle/TruckSDR AALA20041048Frame · corrodedFRAME CORROSION FOUND AT BULKHEAD AFT END OF FORWARD CARGO AT BOTTOM BETWEEN STRINGER 52 RT AND 54 RT AT STATION 39. REPAIRED THE FRAME 39 BULKHEAD IAW ESO 30595 DATED 9/22/04 REPAIR NR 40 531000 3693. (CLOSED)Sep 28, 2004 · N77080 · Airbus A300B4605R · Fuselage Main, FrameSDR CA040924001Vapor Barrier · damaged(CAN) DURING INVEST OF A PNEUMATIC LEAK AT LT A/C PACK DISCHARGE DUCT HEAT EXCHANGER CONNECTOR, FUEL VAPOR BARRIERS FOUND DAMAGED ABOVE THIS AREA. METAL FUEL VAPOR BARRIER HAD DAMAGE OF APPROX 2 SQ FT. FIBER FUEL VAPOR BARRIER PUNCTURED 2 SQ. IN. FUEL VAPORSep 18, 2004 · Airbus A310304 · Air Distribution SystemSDR 04FDEA02674Throttle · obstructedRTO DUE TO LOW POWER NR 2, ENG NR 2 THROTTLE WOULD NOT ADVANCE PAST REF. POINT 30 AND N1 ADVANCED TO 93 PERCENT VS 108 PERCENT REQUIRED. RTO OCCURRED AT 90 KTS. ENT BY: 273927 RPT BY: 096714 SHGN 11SEP04 02:40 GDL U IN WORK, ENT BY: 273927 RPT BY: 27392Sep 10, 2004 · N668FE · Airbus A300F4605R · Power LeverSDR CA040909004Control Unit · malfunctioned(CAN) IN CRUISE, NR 5 SPOILER EXTENDED MOMENTARY FOLLOWED BY SPOILER 5FAULT ON ECAM. SPOILER PANEL RETRACTED ON IT S OWN. SPOILER RESET AFTER LANDING AND CHECKED OK.TROUBLING SHOOTING INDICATED NR 2 EFCU AT FAULT. NR 2 EFCU REPLACED AND DFDR REMOVED AND SENTSep 6, 2004 · Airbus A310304 · Auto Flight SystemSDR AALA20040913Sensor · inoperativeINFLIGHT T 1165/28 GEAR WOULD NOT RAISE AFTER TAKE OFF IN GEAR POSITION SYSTEM 1. TRIED SYSTEM 2 IAW OPERATION MANUAL VOLUME 1. GEAR WOULD NOT RAISE. RETURNED FOR LANDING, LANDED WITHOUT INCIDENT. REPLACED RT BOGIE SYSTEM 1 AND 2 SENSOR AND REPLACED TARGETAug 29, 2004 · N70073 · Airbus A300B4605R · Landing Gear Position and WarningSDR 04FDEA02565Door Frame · gougedAFT CARGO DOOR CUTOUT ON LOWER FWD FRAME, NOTED GOUGES/DAMAGED SURFACE APPROX 13 INCHES LONG. GOUGES RANGE FROM .080 INCH TO .2 INCH. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW A300/600 SRM 53-17-12. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW A300/6Aug 26, 2004 · N677FE · Airbus A300F4605R · Fuselage Main, StructureSDR 04FDEA02539Cargo Track · corrodedMDCC SIDE TRACK AT FR 35 BETWEEN R1 AND R2 HAS LEVEL 1 CORROSION APPROX 1 INCH. REMOVED AND REPLACED SIDE TRACK IAW SRM 51-40-21Aug 21, 2004 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02540Cargo Track · corrodedN00509 MDCC SIDE TRACK AT FR 37 BETWEEN R1 AND R2 HAS LEVEL 1 CORROSION APPROX. 1 INCH. REMOVED AND REPLACED SIDE TRACK ADAPTER TRACK IAW A300 SRM 51-40-20.Aug 21, 2004 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02541Seat Track · corrodedN00466 MAIN CABIN SEAT TRACK (0) AT APPROX FRAME 78 HAS CORROSION ON TOP OF LUGS AND IN BOTTOM OF SCALLOPS. REMOVED CORROSION ON MAIN CARGO TRACK (0) FR 78 IAW SRM 51-74-10. MATERIAL LOSS WAS 0.050 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 105. REPAAug 21, 2004 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02542Seat Track · corrodedN00468 MAIN CABIN SEAT TRACK CORRODED FROM FR47 TO 50, TRACK 3R. REPAIRED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16.Aug 21, 2004 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR AALA20040883Mount · corrodedRT IB AFT ENGINE MOUNT BOLT COUNTER BORE CORRODED. CORROSION REMOVED AND COUNTER BORE TREATED, PRIMED, AND PAINTED IAW ESO 30595 DATED 8/18/04. (CLOSED)Aug 18, 2004 · N70054 · Airbus A300B4605R · Engine Mount SectionSDR AALA20040842Battery Pack · inoperativeBOS EMERGENCY LIGHTS AT FIRST CLASS RIGHT HAND SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS RT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)Aug 13, 2004 · N7055A · Airbus A300B4605R · Emergency LightingSDR 04FDEA02262Fan · out of balanceEN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TROUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9 VIBRATION (AIRFRAME) VIB ON DESCENT. AIRFRAME VIB BETWEEN 80 Jul 28, 2004 · N684FE · Airbus A300B4605R · Turbine Engine Compressor SectionSDR 04FDEA02261Fan · out of balanceIN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TROUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9, VIBRATION (AIRFRAME) VIB ON DESCENT. AIRFRAME VIB BETWEEN 8Jul 28, 2004 · N684FE · Airbus A300B4605R · Turbine Engine Compressor SectionSDR CA040603005Wire · chafed(CAN) AIRCRAFT ARRIVED WITH THE RT OUTER TANK FUEL PUMP NR 1 LOW PRESSURE LIGHT ON. FOLLOWING TROUBLE SHOOTING, THE WIRE FOR NR 1 RT OUTER PUMP WAS FOUND SHORTED IN THE CONDUIT AT REAR SPAR WS 915.0. WIRE WAS REPLACED. MFG WAS ADVISED OF THIS PROBLEM. A CAJun 2, 2004 · Airbus A310304 · Engine Fuel System WiringSDR AALA20040482Seal · leakingSDQ - INFLIGHT T9621/20 SJU-MIA LEFT HAND ENGINE OIL QUANTITY LOSS. AT CRUISE NUMBER 1 OIL QUANTITY SLOWLY DECREASED. PULLED ENGINE TO IDLE AND LEAK CONTINUED. SHUT ENGINE DOWN AT 6 QUARTS. ENGINE WINDMILLED AT ABOUT 15 PERCENT WITHOUT OIL QUANTITY OR PRESApr 21, 2004 · N70073 · Airbus A300B4605R · Turbine Engine Oil SystemSDR CA040413003Access Door · missing(CAN) THE AIRCRAFT ARRIVED AT THE STATION WITH THE MID LAVATORY SERVICING ACCESS DOOR MISSING. THE AIRCRAFT WAS DISPATCHED UNDER CDL AND A NEW DOOR WAS INSTALLED AT THE MAIN BASE. THE LAVATORY SYSTEM WAS CHECKED SERVICEABLE (NO LEAK). SUSPECT PANEL NOT PROPApr 7, 2004 · Airbus A310300 · Fluid Service DoorsSDR CA040405001Wire · malfunctioned(CAN) FLAP JAM OCCURRED AFTER TAKE OFF. AIRCRAFT RETURNED TO THE STATION FOR RECTIFICATION. FLAP SFCC COMPUTER WAS RESET BY MAINTENANCE. FLAP SYSTEM WAS INSPECTED AND OPERATED SEVERAL TIMES WITH NO FAULT FOUND. AIRCRAFT WAS DISPATCH WITH NO FURTHER PROBLEM. AIMar 28, 2004 · Airbus A310300 · Flight Control System WiringSDR CA040324009Rod End · sheared(CAN) DURING TROUBLE SHOOTING A DEFECT ON NR 2 ENGINE REVERSER, LT LOWER SLEEVE NOT STOWING PROPERLY, FOUND THE LOWER JACKSCREW ACTUATORROD END BROKEN. ACTUATOR ASSEMBLY REPLACED AND SYSTEM VERIFIED SERVICEABLE. THIS IS THE SECOND EVENT WITH THE SAME FAILURE WMar 24, 2004 · Airbus A310300 · Engine Thrust ReverserSDR CA040324008Switch · broken(CAN) AIRCRAFT ARRIVED WITH FLAP UNABLE TO RETRACT PAST THE INTERMEDIATE POSITION OF +-5 DEGREES.UPON INVESTIGATION FOUND THE LEFT HAND OUTBOARD VANE JAM DETECTOR UNIT SWITCH SHEARED AND INTERNALLY JAMMED AND BUFFER CRUSHED. THE BRACKET/SWITCH ASSEMBLY WAS REPMar 20, 2004 · Airbus A310300 · Trailing Edge Flap Control SystemSDR CA040324007Rod End · sheared(CAN) DURING ROUTINE INSPECTION, NR 1 ENGINETHRUST REVERSER RT TRANSLATING COWL LOWER JACKSCREW ACTUATOR ROD END FOUND SHEARED IN THREADPORTION OF ROD END. JACKSCREW ACTUATOR ASSEMBLY REPLACED AND SYSTEM VERIFIED SERVICEABLE.Mar 2, 2004 · Airbus A310300 · Engine Thrust ReverserSDR AALA20040221Filter · cloggedJFK INFLIGHT T837/11 AT FLIGHT LEVEL 270 NUMBER 2 ENGINE FUEL CLOG LIGHT CAME ON WITH ECAM MESSAGE. REDUCED POWER TWO TO THREE KNOBS AND LIGHT WENT OUT. RETURNED TO STATION AND LANDED WITHOUT INCIDENT. FOUND FUEL FILTER CLOGGED. REPLACED FUEL FILTER AND AFeb 11, 2004 · N14056 · Airbus A300B4605R · Aircraft Fuel Filter/StrainerSDR AALA20040220Engine · contaminatedMIA INFLIGHT T/1901/10 ON CLIMBOUT NR 2 OIL QUANTITY BEGINS TO DECREASE. AT 20000 FEET OIL QUANTITY WAS AT ZERO AND OIL TEMPERATURE WENT UP TO 154. OIL PRESSURE FLUCTUATED BETWEEN 30 PSI AND 50 PSI. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. AFTER LANDIFeb 10, 2004 · N90070 · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR AALA20040164Pressure Switch · inoperativeSJU INFLIGHT T1522/02, RIGHT INNER NR 2 PUMP FAILURE AND NR 1 PUMP WAS ON MEL. RETURNED TO SJU. LANDED WITHOUT INCIDENT. SUMPED RIGHT INNER NR 2 TANK AND ACCOMPLISHED RIGHT INNER NR 2 PUMP OPERATION. REPLACED THE FUEL PRESSURE SWITCH FOR NR 1 PUMP. SYSTEMFeb 2, 2004 · N7082A · Airbus A300B4605R · Engine Fuel PumpSDR 03FDEA02043Engine · failedDURING ROTATION NR 2 ENG FAILED NO UNUSUAL ENG INDICATIONS. REMOVED AND REPLACED NR 2 ENGINE PER WORK CARD 64T0700-2, ENGINE LEAK AND OPS CHECKS OK. PERFORMED T/O ASSURANCE RUN PER JRH.Dec 2, 2003 · N652FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 03FDEA01795Precooler · crackedCOMPLY WITH EA 6-5452-73216 NACELLES/PYLONS - REPAIR OF CRACKS IN NR 1 ENGINE PYLON PRECOOLER PANEL. COMPLIED WITH EA 6-5452-73216 NACELLES/PYLONS - REPAIR OF CRACKS IN NR 1 ENGINE PYLON PRECOOLER PANEL AT BFM/MAE.Oct 23, 2003 · N660FE · Airbus A300F4605R · Turbine Engine Oil SystemSDR CA031021006Transformer · burned(CAN) DURING FLIGHT, THE CABIN CREW REPORTED AN ELECTRICAL BURNING ODOR IN CABIN AT ROW 13. THE LIGHTS WERE EXTINGUISHED AND THE ODOR DISAPPEARED AFTER 15 MINUTES. MAINTENANCE FOUND THE TRANSFORMER AT ROW 14 ABC SMELLED BURNED. THE PASSENGER SERVICE MODULE Oct 14, 2003 · Airbus A310300 · Equipment/Furnishings WiringSDR AALA20030965Engine · bird ingestionAT 130 KNOTS ON TAKEOFF, THE NR 1 ENGINE BLACK AND WHITE STRIPE NEEDLE FAILED TO ZERO. TAKEOFF CONTROL THEN ENGINE TRIM FAULT LIGHT ILLUMINATED WITH THE TRIM OF NR 1 ENGINE PARAMETERS FLUCTUATED CONSISTENE WITH AN ENGINE PROBLEM. DECLARED AN EMERGENCY AND LASep 7, 2003 · N77080 · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR AALA20030964Pmc · failedAIRCRAFT EN ROUTE AUA TO JFK, PASSING THROUGH FLIGHT LEVEL 210, EXPERIENCED SURGE IN THE NR 1 ENGINE. N1 GREATER THAN 125, EXHAUST GAS TEMPERATURE ABOUT 980 DEGREES. EMERGENCY DECLARED AND COMPLETED A LANDING WITHOUT INCIDENT. AIRCRAFT NOT OVERWEIGHT. REPLACSep 6, 2003 · N34078 · Airbus A300B4605R · Fuel Controlling SystemSDR AALA20030942Engine · failedAIRBUS REPORTED NR 2 ENGINE COMPRESSOR STALL, DECLARES AN EMERGENCY AND LANDS SAFELY. FOUND METAL IN TAILPIPE OF ENGINE. ENGINE CHANGED OUT AT SJU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Sep 2, 2003 · N3075A · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR CA030819001Servo · malfunctioned(CAN) DURING TAKE-OFF ROLL, OUT OF EXETER AND A COUPLE OF TIMES IN FLT, CREW REPORTED RUDDER KICKED, FOLLOWED BY A BANK OF 10 DEGREES. THE YAW AUTOPILOT ACTUATOR WAS REPLACED AND THE SYSTEM WAS CONFIRMED SERVICEABLE AFTER A VERIFICATION FLT.Aug 13, 2003 · Airbus A310300 · Autopilot SystemSDR CA030421001Hose · ruptured(CAN) ON FINAL APPROACH WHEN GEAR SELECTEDDOWNGREEN HYDRAULIC SYSTEM QUANTITY DROPPED TO NEARLY ZERO .DURING INVESTIGATION FOUND THE HYDRAULIC DOWN LINE RUPTURED AT THE UPPER RIGHT HAND MAIN LANDING GEAR SWIVEL AREA. LINE WAS REPLACED AND SYSTEM TESTED SERVICEApr 16, 2003 · Airbus A310304 · Landing Gear Retraction/Extension SystemSDR CA030321002Tube · damaged(CAN) DURING FLIGHT HYDRAULIC RESERVOIR LOW LEVEL APPEARED ON GREEN SYSTEM. AFTER INVESTIGATION A PIN HOLE WAS FOUND ON THE LT WING SPOILER PRESSURE TUBE. TUBE ASSY WAS REPLACED AS M/M AND SYSTEM SERVICED AIRCRAFT WAS RETURNED TO SERVICE. CAUSE OF FAILURE ISMar 20, 2003 · Airbus A310300 · Hydraulic System, MainSDR CA030214009Bolt · loose(CAN) DURING THE A-01 CHECK, RT MAIN LANDING GEAR, EMERGENCY BRAKE MANIFOLD WAS SUSPECTED TO BE LEAKING. INSPECTION FOUND THE ALTERNATE BRAKE RETURN ACCUMULATOR LOOSE ON THE MANIFOLD, DUE TO THE FACT THAT THE BOLTS INSTALLED TO SECURE THE ACCUMULATOR WERE NOT Feb 10, 2003 · Airbus A310300 · Fasteners
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